CZ-3B R/B, 63158 (Decayed)
Orbit data source: Space-Track
CZ-3B R/B, 63158 was space debris in LEO originally from a launch on Sun, 09 Mar 2025 UTC launched from the Xichang Space Center, China (XSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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63158 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-3B R/B
1 63158U 25045B 25219.67477155 .98136556 -71417-5 62121-2 0 9993
2 63158 19.1569 312.7507 1541275 25.9292 125.2963 12.90064588 4662Epoch: 2025-08-07T16:11Z
TLE epoch observation values (Epoch: 2025-08-07T16:11:40.261Z)
Latitude
5.17494°
Longitude
-81.64556°
Altitude
2,088.223 km
Speed
6.503 km/s
True Right ascension
07h 50m 49s
True Declination
5° 08' 56"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:15:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,490.637 km
Perigee altitude
121.883 km
Semi-major axis
7,684.397 km
Eccentricity
0.15413
Inclination
19.1569°
RAAN
312.7507°
Arg. of periapsis
25.9292°
True anomaly
138.1556°
Mean anomaly
125.2963°
Eccentric anomaly
131.87208°
Mean motion
3.22202 °/min
Orbital period
111.73 mins
BSTAR
0.0062121
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Other satellites on launch #45 in the year 2025 (2025-03-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-3B R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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